HYDRAULIC SYSTEM FOR LANDING GEARS OF AIRCRAFT Russian patent published in 1995 - IPC

Abstract RU 2032596 C1

FIELD: aviation, aircraft. SUBSTANCE: hydraulic system has hydraulic cylinders for landing gear legs 1, side shields control hydraulic cylinders 2, brake shoes control hydraulic cylinders 3, brake shoes switch 6 with a working chamber and lines for extension and retraction of landing gear, control valve switch 7 and shut-off valve 8. Control valve switch 7 is located on the above extension and retraction lines; the working chamber of switch 6 is connected to the extension line. EFFECT: safer take-off and landing. 1 dwg

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RU 2 032 596 C1

Authors

Taranenko N.N.

Dates

1995-04-10—Published

1991-06-01—Filed